SCOUT X-4 R/B
Satellite information SCOUT X-4 R/B
| Spacetrack Directory Name | SCOUT X-4 R/B |
| Follow SCOUT X-4 R/B | SCOUT X-4 R/B Tracker |
| Pass predictions SCOUT X-4 R/B | Pass predictions SCOUT X-4 R/B |
| Orbit launches |
1964-06-04 (62 years ago)
|
| Days in orbit | 22787 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 833 km |
| Apogee | 891 km |
| Orbit slope (inclination) | 90.45° |
| Laps per day | 14 |
| Height SCOUT X-4 R/B | 868.87 km |
Additional information SCOUT X-4 R/B
SCOUT X-4 R/B, 809 is space debris in LEO originally from a launch on Thu, 04 Jun 1964 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite SCOUT X-4 R/B Date of exalting 04.06.1964y. Average height of ISS SCOUT X-4 R/B hundred 868.87 km. Average velocity SCOUT X-4 R/B is 26710.14 km/h. Inclination SCOUT X-4 R/B satellite 90.45°.TLE
Average velocity SCOUT X-4 R/B
Average inclination SCOUT X-4 R/B
Mean right ascension of the ascending node (RAAN) SCOUT X-4 R/B
Mean argument of perigee SCOUT X-4 R/B
Mean semi-major axis of the orbit SCOUT X-4 R/B
Mean orbital eccentricity SCOUT X-4 R/B
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